# TCDS 2A8: Lavia Argentina S.A. (Laviasa)

- Type: Type certificate data sheet
- Status: Current
- Holder: Lavia Argentina S.A. (Laviasa)
- Revision: 23
- Revised: July 14, 2021
- Product: Aircraft, Small Airplane
- Certification basis: CAR 3
- Registered aircraft: 453, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/c2/19/c219e526135fde6a01cec3afc4b60491daacbd6af148dbc03de125ae8dd4ebbc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/32C3CC4AE2153FBB862587130048EF78.0001
- Page: https://openairdocs.org/tcds/2A8

## Models (3)

As the data sheet lists them.

- PA-25-235
- PA-25 (Pawnee)
- PA-25-260

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
Page No. 1 2 3 4 5 6 7 8 
Rev. No. 22 20 20 20 20 20 20 23 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
2A8 
Revision 23 
LAVIA S.A. 
PA-25 
PA-25-235 
PA-25-260 
 
July 14, 2021 
TYPE CERTIFICATE DATA SHEET 2A8 
 
This data sheet which is part of Type Certificate No. 2A8 prescribes conditions and limitations under which the 
product for which the Type Certificate was issued meets the airworthiness requirements of the Civil Air Regulations 
and Federal Aviation Regulations. 
 
Type Certificate Holder LAVIA ARGENTINA S.A. (LAVIASA) 
 Avenida Colo
 n 412, P.B. Dpto B 
 C.P. 5500, Mendoza 
 Repu
 blica Argentina 
 
Type Certificate Record of  LATINOAMERICANA DE AVIACION (LAVIA S.A.) changed its trade name to  
Name Change to LAVIA ARGENTINA S.A. (LAVIASA) on February 29, 2008 
 (TC reissued March  25, 2008)  
 
I.- Model PA-25, 1 PCLM   (Normal Category),  Approved January 6, 1959. 
 
Engine Lycoming O-320-A1A, O-320-A2A with carburetor setting 10-3678-11 or 
 Lycoming O-320-A2B with carburetor setting 10-3678-32. 
 
Fuel 80/87 minimum grade aviation gasoline 
 
Engine Limits For all operations, 2700 r.p.m.     (150 hp.)  
 
Propeller and Propeller Limits McCauley 1A170-GM or Sensenich M74DM 
 Static r.p.m. at maximum permissible throttle setting: 
  Not over 2575 r.p.m., not under 2475 r.p.m. 
  No additional tolerance permitted. 
 Diameter:  Not over 74 inches, not under 72.5 inches 
 Spinner required:  Piper Drawing No. 14422 
 
Airspeed Limits   (CAS) Vne Never exceed 136 mph (118 knots) 
 Vno Maximum structural cruising 108 mph   (94 knots) 
 Vp Maneuvering 107.5 mph   (93 knots) 
 Vfe Flaps extended   95 mph   (83 knots) 
 
Center Gravity Range (+11.70) to (+15.25) at 2300 lb. 
 (+9.98) to (+15.25) at 1600 lb. or less 
 Straight line variation between points given. 
 
Empty Weight  
        Center of Gravity Range None 
 
Datum Leading edge of wing 
 
Leveling Means Top longerons in cockpit bay

2A8 Page 2 of 8 
 
Maximum Weight 2300 lb. 
 
No. of Seats 1 at  (+59) 
 
Maximum Cargo 800 lb. at  (+14) 
 
Fuel Capacity 40 gallons at  (-14.9) (one fuselage tank) 
 See NOTE 1 for data on system fuel. 
 
Oil Capacity 8 quarts at (-47) (6 quarts usable) 
 See NOTE 1 for data on system oil. 
 
Control Surface Movements Wing Flaps   Down 57° 
 Aileron Up 23° Down 23° 
 Elevator Up 28° Down 15° 
 Rudder Right 25° Left 25° 
 
Manufacturer's Serial Numbers 25-1 through 25-731 
 
 
II. - Model PA-25-235,   1  PCLM  (Normal Category),   Approved October 12, 1962. 
 
Engine Lycoming O-540-B2B5 or O-540-B2C5 with carburetor setting #10-4404-1 
 
Fuel 80/87 minimum grade aviation gasoline 
 
Engine Limits For all operations, 2575 r.p.m.  (235 hp.) 
 
Propeller and Propeller Limits 1. McCauley 1A200-FA (Eligible on S/N 25-02;  25-2000 through 25-5521;  
  25-7305522 through 25-8156024; and LA-235-99501 and up) 
  Static r.p.m. at maximum permissible throttle setting: 
   Not over 2350 r.p.m., not under 2250 r.p.m. 
   No additional tolerance permitted. 
  Diameter:  Not over 84 inches, not under 82.3 inches 
  Spinner required:  Piper Drawing No. 64336. 
 
 2. McCauley 1P235-AFA (Eligible on S/N 25-02, and 25-2000 through  
  25-4171): 
  Static r.p.m. at maximum permissible throttle setting: 
   Not over 2500 r.p.m., not under 2400 r.p.m. 
   No additional tolerance permitted. 
  Diameter:  Not over 84 inches, not under 82.3 inches 
  Spinner required:  Piper Drawing No. 14422 
 
Airspeed Limits   (CAS) Vne Never exceed 156 mph (135 knots) 
 Vno Maximum structural cruising 124 mph (108 knots) 
 Vp Maneuvering 120 mph (104 knots) 
 Vfe Flaps extended 109 mph (  95 knots) 
 
Center Gravity Range (+88.4) to (+90.3) at 2900 lb. 
 (+85.6) to (+90.3) at 1793 lb. or less 
 Straight line variation between points given. 
Empty Weight 
          Center of Gravity Range None 
 
Datum 78 inches forward of leading edge of wing 
 
Leveling Means Top longerons in cockpit bay 
 
Maximum Weight 2900 lb.

Page 3 of 8 2A8 
 
Number of Seats 1 at  (+135) 
 
Maximum Cargo 1200 lb. at  (+93) 
 
Fuel Capacity For S/N 25-02, and 25-2000 through 25-3384: 
  42 gallons at  (+63) (one fuselage tank) 
 For S/N 25-3385 through 25-5521, and 25-7305522 through 25-7405572, and  
 LA-235-99501 and up:: 
  38 gallons at  (+63) (one fuselage tank) 
 For S/N 25-7405573 through 25-8156024: 
  36 gallons at  (+102) (two wing tanks) 
 See NOTE 1 for data on system fuel. 
 
Oil Capacity 12 quarts at  (+30) (9¼ quarts usable) 
 See NOTE 1 for data on system oil. 
 
Control Surface Movements  Wing Flaps   Down 57° 
 Aileron Up 23° Down 23° 
 Elevator Up 28° Down 15° 
 Rudder Right 25° Left 25° 
 
Manufacturer's Serial No. 25-02;  25-2000 through 25-5521;  and 25-7305522 through 25-8156024, produced by 
Piper Aircraft Corp.; LA-235-99501 and up produced by LAVIA S.A. 
 See NOTE 5 for airworthiness certification eligibility in the United States. 
 
III. - Model PA-25-260,   1 PCLM  (Normal Category Only),   Approved April 19, 1967. 
 
Engine Lycoming O-540-G1A5 or O-540-G2A5 with carburetor setting #10-4404-1 
 
Fuel 100/130 minimum grade aviation gasoline 
 
Engine Limits For all operations, 2700 r.p.m.  (260 hp.) 
 
Propeller and Propeller Limits 1. McCauley 1A200-FA 
  Static r.p.m. at maximum permissible throttle setting: 
   Not over 2425 r.p.m., not under 2325 r.p.m. 
   No additional tolerance permitted 
  Diameter:  Not over 84 inches, not under 82.3 inches 
  Spinner required:  Piper Drawing No. 64336 
 
 2. Hartzell constant speed model HC-C2YK-1( )/8477-0 
  (Eligible on O-540-G1A5 engine only) 
  Pitch setting at 30" station:  High 32.0°, Low 11.8° 
  Diameter:  Not over 84.0 inches, not under 83.0 inches 
  Governor assembly:  Hartzell F-4-4( ) 
  Spinner:  None approved 
 
 3. McCauley constant speed model B2D34C16-( )/84 HF-0 
  (Eligible on O-540-G1A5 engine only) 
  Pitch setting at 30" station:  High 27.0°, Low 11.0° 
  Diameter:  Not over 84.0 inches, not under 82.5 inches 
  Governor assembly:  McCauley C290D2( )/T10 
  Spinner:  None approved 
 
Airspeed Limits   (CAS) Vne Never exceed 156 mph (135 knots) 
 Vno Maximum structural cruising 124 mph (108 knots) 
 Vp Maneuvering 120 mph (104 knots) 
 Vfe Flaps extended 109 mph (  95 knots) 
 
Center Gravity Range (+88.4) to (+90.3) at 2900 lb. 
 (+85.6) to (+90.3) at 1793 lb. or less 
 Straight line variation between points given.

2A8 Page 4 of 8 
 
Empty Weight 
   Center of Gravity Range None 
 
Datum 78 inch forward of leading edge of wing 
 
Leveling Means Top longerons in cockpit bay 
 
Maximum Weight 2900 lb. 
 
Number of Seats 1 at  (+135) 
 
Maximum Cargo 1200 lb. at (+93) 
 
Fuel Capacity For S/N 25-4415 through 25-5521, and 25-7305522 through 25-7405572 and  
 LA-260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up: 
  38 gallons at (+63) (one fuselage tank) 
 For S/N 25-7405573 through 25-8156024: 
  36 gallons at (+102) (two wing tanks) 
 See NOTE 1 for data on system fuel. 
 
Oil Capacity 12 quarts at  (+30) (9¼ quarts usable) 
 See NOTE 1 for data on system oil. 
 
Control Surface Movements Wing Flaps   Down 57° 
 Aileron Up 23° Down 23° 
 Elevator Up 28° Down 15° 
 Rudder Right 25° Left 25° 
 
Manufacturer's Serial Numbers 25-4415 through 25-5521, and 25-7305522 through 25-8156024, produced by Piper 
Aircraft; LA-260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up, 
produced by LAVIA S.A. 
 See NOTE 5 for airworthiness certification eligibility in the United States. 
 
DATA PERTINENT TO ALL MODELS 
Certification Basis CAR 3 effective May 15, 1956, Amendment 3-1, April 1, 1957. 
 Type Certificate No. 2A8 issued January 5, 1959. 
 Date of Application for Type Certificate May 28, 1957. 
 
Production Basis For aircraft models PA-25-235 S/N LA-235-99501 and up,  and PA-25-260  
 S/N LA-260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up, production 
under type certificate only. 
 
Equipment The basic required equipment prescribed in the applicable airworthiness regulations (see 
Certification Basis) must be installed in the aircraft for certification.  In addition, the 
following items of equipment are required: 
 1. FAA Approved Airplane Flight Manual: 
  (a) Issue dated May 20, 1959, required for S/N 25-1 and 25-2. 
  (b) Issue dated July 9, 1959, revised February 23, 1960, for S/N  
   25-3 through 25-1999. 
  (c) Issue dated October 12, 1962, including Revision No. 1, dated 
   November 20, 1962, for Model PA-25-235, S/N 25-02, and 
   25-2000 through 25-2761. 
  (d) Issue dated October 12, 1962, including Revision No. 1, dated  
   November 20, 1962, and No. 2 dated July 20, 1964, for Model PA-25-235,  
   S/N 25-2762 through 25-2985. 
  (e) Issue dated October 12, 1962, including Revision No. 1, 2, 3 and 4 for  
   Model PA-25-235, S/N 25-2986 through 25-3384. 
   
 
  (f) Issue dated October 12, 1962, including Revision Nos. 1, 2, 3, 4, and 5 for  
   Model PA-25-235, S/N 25-3385 through 25-4171.

Page 5 of 8 2A8 
 
 
Equipment, continued 
1. FAA Approved Flight Manual, continued  
(g) Issue dated October 12, 1962, including Revisions Nos. 1, 2, 3, 4, 5, 6, 7, 8, 9  
   and 10 for Model PA-25-235, S/N 25-4172 through 25-5521, and 25-7305522 
   through 25-7405572 and LA-235-99501 and up. 
  (h) Issue dated April 19, 1967, including Revision No. 1 required for  
   Model PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 
   25-7405572 and LA-260-98001, LA-260-99002, LA-260-99003, LA-260-
99005 and up. 
  (i) Issue dated February 7, 1974, required for Models PA-25-235 and PA-25-260,  
   S/N 25-7405573 through 25-8156024.  
 
 2. Stall warning indictor device per Piper Drawing Nos. 61093 and 61128 on  
  PA-25, S/N 25-3 through 25-1999;  Piper Drawing Nos. 64031 and  
  64253 on PA-25-235, S/N 25-02, and 25-2000 through 25-4171;  Piper  
  Drawing Nos. 64031 and 64884 on PA-25-235, S/N 25-4172 through  
  25-4414, and on PA-25-235 or PA-25-260, S/N 25-4415 through 25-5521 and  
  25-7305522 through 25-8156024; LA-235-99501 and up; LA-260-98001, LA-260-
99002, LA-260-99003, LA-260-99005 and up. 
 
NOTE 1 Current weight and balance report, including list of equipment included in certificated empty weight and 
loading instructions when necessary, must be provided for each aircraft at time of original certification.   
 
The certificated empty weight and the corresponding  center of gravity locations must include undrainable system oil (not 
included in oil capacity) and unusable fuel as noted below:    
 
 Mod  Model PA-25: Fuel 14  lb. at (-23)   
  Oil 3.2 lb. at (-47)   
        
 Mod  Model PA-25-235, S/N 25-02, 
  25-     25-2000 through 25-3384: 
 
Fuel 
 
18  lb. 
 
at 
 
(+55) 
  
  Oil 5.2 lb. at (+30)   
        
 Mod  Model PA-25-235, S/N 25-3385 
         through 25-5521, and 25-7305522 
         through 25-7405572; 
  LA-235-99501 and up: 
 
 
 
Fuel 
 
 
 
12 lb. 
 
 
 
t 
 
 
 
(+55) 
  
  Oil  5.2 lb. at (+30)   
        
     M  Model PA-25-260, S/N 25-4415 
     t    through 25-5521, and 25-7305522 
     t    through 25-7405572; 
  LA    LA-260-98001, LA-260-99002, 
 LA- LA-260-99003, LA-260-99005 and up  
 
 
 
Fuel 
 
 
 
12 lb. 
 
 
 
at 
 
 
 
(+55) 
  
  Oil  5.2 lb. at (+30)   
        
 Mod  Models PA-25-235 and PA-25-260, 
  S/N    25-7405573 through  
  25-     25-8156024: 
 
 
Fuel 
 
 
15 lb. 
 
 
at 
 
 
(+110) 
  
  Oil  5.2 lb. at (+30)   
 
NOTE 2. The following placards must be displayed: 
 (a) In front and in clear view of the pilot: 
  (1) On Model PA-25, S/N 25-1 through 25-1999: 
   "THIS AIRPLANE MUST BE OPERATED IN THE NORMAL CATEGORY IN COMPLIANCE  
   WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS,   
  MARKINGS, AND MANUAL.  ACROBATIC MANEUVERS (INCLUDING SPINS)  
   PROHIBITED.  FOR RESTRICTED CATEGORY OPERATION, REFER TO ADDITIONAL  
   LIMITATIONS."

2A8 Page 6 of 8 
 
 (2) On Model PA-25-235, S/N 25-02, 25-2000 through 25-2761: 
   "THIS AIRPLANE MUST BE OPERATED IN THE RESTRICTED CATEGORY IN  
   COMPLIANCE WITH OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS  
   AND MARKINGS.  ACROBATIC MANEUVERS (INCLUDING SPINS) PROHIBITED." 
  NOTE 2(a)(2), continued         
        (2) On Model PA-25-235, S/N 25-02, 25-2000 through 25-2761, continued  
 
   Model PA-25-235, S/N 25-02 and 25-2000 through 25-2761 are also eligible for Multiple 
   Airworthiness Certification when all placards are revised to the configuration of S/N  
   25-2762 through 25-5521, and 25-7305522 through 26-8156024.  Airplane Flight Manual  
   equipment Item 1(d) required in lieu of Item 1(c). 
 
  (3) On Model PA-25-235, S/N 25-2762 through 25-4414; on Model PA-25-235 or PA-25-260, S/N 
   25-4415 through 25-5521, and 25-7305522 through 25-8156024; LA-235-99501 and up and  
   LA-260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up: 
 
   "THIS AIRPLANE MUST BE OPERATED IN THE RESTRICTED CATEGORY IN  
   COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF  
   PLACARDS AND MARKINGS.  ACROBATIC MANEUVERS (INCLUDING SPINS)  
   PROHIBITED.  FOR NORMAL CATEGORY OPERATION, REFER TO FLIGHT MANUAL." 
 
 (b) On hopper: 
   Model PA-25   "800 lb. maximum" 
   Model PA-25-235 "1200 lb. maximum" 
   Model PA-25-260 "1200 lb. maximum" 
 
 (c)  Models PA-25-235 and PA-25-260 - On check list above instrument panel: 
"WINDOWS CLOSED" 
 
 (d) Model PA-25-235, S/N 25-2762 through 25-4414; and LA-235-99501 and up and Model PA-25-235 or 
PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 25-8156024 and Model PA-25-
260, S/N  LA260-98001, LA-260-99002, LA-260-99003, LA-260-99005 and up - On the instrument 
panel in full view of the pilot: 
"ROUGH AIR OR MANEUVERING SPEED 120 M.P.H." 
 
 (e)   On safety panel above instrument panel in full view of pilot: 
  (1)Model PA-25-235, S/N 25-02, 25-2000 through 25-3384: 
  "UNUSABLE FUEL 3 GALLONS.  WHEN FUEL QUANTITY INDICATOR READS ZERO, FUEL 
  REMAINING IN TANK CANNOT BE USED SAFELY IN FLIGHT." 
  (2)Model PA-25-235, S/N 25-3385 through 25-4414 and LA-235-99501 and up;  Model PA-25-235 or 
         PA-25-260, S/N 25-4415 through 25-5521, and 25-7305522 through 25-7405572; and  Model  
  PA-25-260, S/N LA-260-98001 and up: 
  "UNUSABLE FUEL 2 GALLONS.  WHEN FUEL QUANTITY INDICATOR READS ZERO,  
  FUEL REMAINING IN TANK CANNOT BE USED SAFELY IN FLIGHT." 
  (3)Model PA-25-235 or PA-25-260, S/N 25-7405573 through 25-8156024:  
  "UNUSABLE FUEL 2.5 GALLONS.  WHEN FUEL QUANTITY INDICATOR READS ZERO,  
  FUEL REMAINING IN TANK CANNOT BE USED SAFELY IN FLIGHT." 
 
 (f) On Models PA-25-235 and PA-25-260 - On instrument panel in clear view of the pilot: 
"NO SMOKING" 
 
 (g) On Model PA-25-235, S/N 25-2762 through 25-4414;  and Model PA-25-235 or PA-25-260, S/N 
 25-4415 through 25-5521, and 25-7305522 through 25-8156024 - In front and in clear view of the   
  pilot: 
 "STALL WARNING SYSTEM INOPERATIVE WHEN MASTER SWITCH IS OFF." 
 
 (h) On Models PA-25-235 and PA-25-260, S/N 25-7405573 through 25-8156024 - Above and near the fuel  
  quantity gauge: 
 "FUEL CAPACITY 36 GALLONS"

Page 7 of 8 2A8 
 
  
 (i) On Models PA-25-235 and PA-25-260, S/N 25-7405573 through 25-8156024 - Adjacent to low fuel  
  level light on auxiliary instrument panel: 
"LOW FUEL WARNING" 
 
NOTE 3. The Model PA-25, S/N 25-2 through 25-1999 (Restricted Category) is the same as the Normal Category  
 PA-25 except for installation of spray or dust dispensing equipment.  Conversion to duster or sprayer 
configuration may be accomplished using Piper Instructions, Section XVI of Report 1019.  When operating 
in the Restricted Category, FAA Type Certificate Data Sheet No. 2A10 will apply. 
 
NOTE 4. (a)Model PA-25-235, S/N 25-2000 through 25-2761 are eligible for Multiple Airworthiness Certification 
when all placards are revised to the configuration of S/N 25-2762 through 25-5521, and 25-7305522 through  
 25-8156024.  Airplane Flight Manual equipment Item 1(d) required in lieu of Item 1(c). 
 
 (b)Model PA-25-235, S/N 25-2762 through 25-2985 are eligible for Multiple Airworthiness Certification in 
the Restricted Category and Normal Category in accordance with CAR 8.21 and Conversion Instructions, 
Section XVI of Piper Report VB-7, Revision No. 2, dated October 5, 1964.  When operating in the 
Restricted Category, Type Certificate Data Sheet No. 2A10 shall apply.  When operating in the Normal 
Category, Type Certificate Data Sheet No. 2A8 shall apply. 
 
 (c)Model PA-25-235, S/N 25-2986 through 25-4414 and Model PA-25-235 or PA-25-260, S/N 25-4415 
through 25-5521, and 25-7305522 through 25-8156024 are eligible for Multiple Airworthiness Certification 
in the  Restricted Category and Normal Category in accordance with CAR 8.21 and Conversion Instructions, 
Section III of Piper Report VB-42, Revision No. 6, dated February 22, 1967.  When operating in the 
Restricted Category, Type Certificate Data Sheet No. 2A10 shall apply.  When operating in the Normal 
Category, Type Certificate Data Sheet No. 2A8 shall apply. 
 
NOTE 5 The following S/N are not eligible for Airworthiness Certification in the United States: 
 
 25-4894, 25-5027, 25-5030, 25-5033, 25-5057, 25-5066, 25-5069, 25-5072, 25-5075, 25-5097, 25-5100,  
      25-5102, 25-5106, 25-5269, 25-5271, 25-5273, 25-5275, 25-5284 through 25-5293, 25-5315, 25-5316,  
      25-5318, 25-5320, 25-5454, 25-5455, 25-5456, 25-5457,  
 25-7305528, 25-7305530, 25-7305532,  
 25-7405591, 25-7405596, 25-7405613, 25-7405620, 25-7405631, 25-7405642, 25-7405652, 25-7405658, 
25-7405662, 25-7405672, 25-7405679, 25-7405686, 25-7405690, 25-7405692, 25-7405694, 25-7405696, 
25-7405698, 25-7405701, 25-7405704, 25-7405705, 25-7405706, 25-7405708, 25-7405714, 25-7405716, 
25-7556030, 25-7556035, 25-7556040, 25-7556045, 25-7556050, 25-7556052, 25-7556057, 25-7556062,  
 25-7556065, 25-7556067, 25-7556069, 25-7556071, 25-7556073, 25-7556075, 25-7556077, 25-7556080, 
 25-7556090, 25-7556095, 25-7556100, 25-7556105, 25-7556110, 25-7556115, 25-7556120, 25-7556125,  
 25-7556135, 25-7556140, 25-7556145, 25-7556150, 25-7556153, 25-7556159, 25-7556162, 25-7556166,  
 25-7556226, 25-7556227, 25-7556228, 25-7556229, 25-7556230, 25-7556231, 25-7556232, 25-7556233, 
 25-7656078, 25-7656091,  
 25-7756072 through 25-7756081, 25-7756087 through 25-7756095, 
 25-7856001 through 25-7856004, 25-7856006, 25-7856008, 25-7856010, 25-7856012, 25-7856016,  
 25-7856018, 25-7856020, 25-7856022, 25-7856032, 25-7856034, 25-7856036, 25-7856038, 25-7856043,  
 25-7856045, 25-7856047, 25-7856049, 25-7856055, 25-7856057, 25-7856063, 25-7856065, 25-7856066,  
 25-7856067, 25-7856069, 25-7856071,  
 25-7956004, 25-7956006, 25-7956009 through 25-7956012,  
 25-7956014, 25-7956016, 25-7956019, 25-7956020, 25-7956022, 25-7956025, 25-7956027, 25-7956029, 
 25-7956031, 25-7956033, 25-7956036, 25-7956038, 25-7956041, 25-7956042,  
 25-8056004, 25-8056005, 25-8056008, 25-8056009, 25-8056011, 25-8056013, 25-8056016, 25-8056018,  
 25-8056021, 25-8056022, 25-8056026, 25-8056028, 25-8056041, 25-8056043, 25-8056046, and 25-8056048.

2A8 Page 8 of 8 
 
 
NOTE 6:  Import Requirements:   
(a) United States airworthiness certificate may be issued on the basis of Argentina  
Certificate of Airworthiness for Export signed by a representative of Direción Nacional de Aeronavegabilidad  
containing the following statement:  “The aircraft conforms to its U. S. type design (Type Certificate No 2A8)  
and is in a condition for safe operation.” 
 (b) The U. S. airworthiness certification basis for aircraft type certificated under 14 CFR Part 21 section 21.29 
and exported by the country of manufacture is section 21.183(c) or 21.185(c).  
(c)The U. S. airworthiness certification basis for aircraft type certificated under 14 CFR Part 21 section  
21.29 and exported from countries other than the country of manufacture (e.g., third part country) is section  
21.183(d) or 21.185(b).  
 
Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new 
and used aircraft based on the scope of the agreement, to identify any required statements by the exporting 
authority on the export certificate of airworthiness (or equivalent document), and for procedures for 
coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2, 
Airworthiness Certification of Aircraft, for requirements for issuance of an airworthiness certificate for 
imported aircraft. 
 
 
     .....END.....
```

## ADs (1, in force first)

- [AD 93-10-06](https://openairdocs.org/ad/93-10-06) (historical): Corroded Wing Lift Struts or Cracked Forks · Piper Aircraft, Inc., The New J-2, J-3, J4 and 28 more. Effective Jul 9, 1993

## Registered aircraft by registry model (OpenAirDocs)

- [Piper PA-25-235](https://openairdocs.org/model/piper-pa-25-235): 347 aircraft (registry code 7102504)
- [Piper PA-25](https://openairdocs.org/model/piper-pa-25): 59 aircraft (registry code 7102502)
- [Piper PA-25-260](https://openairdocs.org/model/piper-pa-25-260): 47 aircraft (registry code 7102508)
- [Piper/Midwest Air Center PA-25-235](https://openairdocs.org/model/piper-midwest-air-center-pa-25-235): 0 aircraft (registry code 7102505)

## STCs approved under this data sheet (123, first 50)

- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes.. Concorde Battery Corporation
- [STC SA1892WE](https://openairdocs.org/stc/SA1892WE): Installation of hydraulic system. Texas Transland LLC
- [STC SA521WE](https://openairdocs.org/stc/SA521WE): Swathmaster dust and spray attachment.. Texas Transland LLC
- [STC SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system.. Shady Aviation LLC
- [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc.
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft.. Michelin North America Inc.
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC
- [STC SA00954WI](https://openairdocs.org/stc/SA00954WI): Installation of Concorde RG Series Batteries in Piper Single Engine Airplanes.. Aero-Mach Wilco LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc.
- [STC SA1151NW](https://openairdocs.org/stc/SA1151NW): Installation of the Flight Grip Model 135 Control Stick Grip. Air Products & Parts LLC
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies
- [STC SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights.. Whelen Aerospace Technologies
- [STC SA04112CH](https://openairdocs.org/stc/SA04112CH): Installation of Appareo Systems, LLC Stratus ESG ADS-B transponder. Appareo Systems LLC.
- [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments
- [STC SA04424AT](https://openairdocs.org/stc/SA04424AT): Installation of Continental Motors, Inc. (CMI) Shower-of-Sparks  Starting Vibrator Booster Systems. Continental Motors, Inc.
- [STC SA00024NY](https://openairdocs.org/stc/SA00024NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [STC SA02212AK](https://openairdocs.org/stc/SA02212AK): Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Seaplanes North LLC
- [STC SA2586NM](https://openairdocs.org/stc/SA2586NM): Installation of J.P. Instruments temperature monitoring systems.. J P Instruments
- [STC SA02428SE](https://openairdocs.org/stc/SA02428SE): Installation of an Air Stream Switch for an electric time recording device on non-pressurized aircraft. Henry F Rogers/David E Polley
- [STC SA01734SE](https://openairdocs.org/stc/SA01734SE): Application of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.. Andrew D. Humphrey
- [STC SA441SW](https://openairdocs.org/stc/SA441SW): Installation of Flexsteel Landing Gear. Martin Slone
- [STC SA725SW](https://openairdocs.org/stc/SA725SW): Metal covered fuselage and fin. Martin Slone
- [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC
- [STC SA00149BO](https://openairdocs.org/stc/SA00149BO): Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1. Aircraft Components Inc
- [STC SA03658AT](https://openairdocs.org/stc/SA03658AT): Installation of a Voice Alert System to incorporate as primary annunciators for stall and gear warnings. Aircraft Components Inc
- [STC SA00478CH](https://openairdocs.org/stc/SA00478CH): Installation of Cooper Superflite 102 Fabric.. Aviation Products Systems Inc.
- [STC SA4305WE](https://openairdocs.org/stc/SA4305WE): Installation of GAR-AERO wheel adapters and tundra type tires on the main landing gear. Seaplanes North LLC
- [STC SA01669CH](https://openairdocs.org/stc/SA01669CH): Installation of Challenger Reusable Air Filter. Challenger Aviation Products Inc.
- [STC SA00992AT](https://openairdocs.org/stc/SA00992AT): Installation of a wing forward spar fuselage attachment cluster and cross tube.. Aerospace Welding Minneapolis Inc.
- [STC SA10682SC](https://openairdocs.org/stc/SA10682SC): Installation of alternator and voltage regulator. Hartzell Engine Technologies, LLC
- [STC SA02283SE PAGE 1](https://openairdocs.org/stc/SA02283SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc.
- [STC SA02402SE PAGE 1](https://openairdocs.org/stc/SA02402SE%20PAGE%201): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc.
- [STC SA3531NM](https://openairdocs.org/stc/SA3531NM): Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP). Bogert Aviation
- [STC SA01154AT](https://openairdocs.org/stc/SA01154AT): Installation of the wing forward spar fuselage attachment assembly reinforcement.. Aerial Banners Mods LLC
- [STC SA01359AT](https://openairdocs.org/stc/SA01359AT): Installation of wing forward spar fuselage attachment assembly reinforcement.. Aerial Banners Mods LLC
- [STC SA02128LA](https://openairdocs.org/stc/SA02128LA): Installation of aileron and flap hinge repair bushings. Univair Aircraft Corporation
- [STC SA00432SE](https://openairdocs.org/stc/SA00432SE): Installation of EGT 701 series fuel flow instrument.. J P Instruments
- [STC SA00861SE](https://openairdocs.org/stc/SA00861SE): Installation of J.P. Instruments (JPI) fuel flow indicating system. J P Instruments
- [STC SA01026SE](https://openairdocs.org/stc/SA01026SE): Improved fuel gascolator assembly.. Steve's Aircraft
- [STC SA02825NY PAGE 1](https://openairdocs.org/stc/SA02825NY%20PAGE%201): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc.
- [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation
- [STC SA2515NM](https://openairdocs.org/stc/SA2515NM): Installation of Hoffmann HO 4/27 BHM-185 fixed pitch propeller in accordance with FAA Mile High Gliding, Inc. Report No. 2501 dated June 18, 1984, or later FAA approved revision.  FAA Approved Airplane Flight Manual supplements are required for normal category as listed in the Approved Model List.. Mile High Gliding Inc.
- [STC SA316BO](https://openairdocs.org/stc/SA316BO): Modification of a fuel system by the installation of a fuel pump and auxiliary fuel tank for the transfer of fuel from the auxiliary tank to the main tank.. Simmons Aviation Services LLC

All 123: https://openairdocs.org/tcds/2A8/stcs.md

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